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Design optimization workflow and performance analysis for contoured endwalls of axial turbines

机译:轴流式涡轮机轮廓壁的设计优化工作流程和性能分析

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摘要

Advances in computer-based optimization techniques can be used to enhance the efficiency of energy conversions processes, such as by reducing the aerodynamic loss in thermal power plant turbomachines. One viable approach for reducing this flow energy loss is by endwall contouring. This paper implements a design optimization workflow for the casing geometry of a 1.5 stage axial turbine, towards mitigating secondary flows. Two different parametric casing surface definitions are used in the optimization process. The first method is a new nonaxisymmetric casing design using a novel surface definition. The second method is an established diffusion design technique. The designs are tested on a three-dimensional axial turbine RANS model. Computer-based optimization of the surface topology is demonstrated towards automating the design process. This is implemented using Automated Process and Optimization Workbench (APOW) software. Kriging is used to accelerate the optimization process. The optimization and its sensitivity analysis give confidence that a good predictive ability is obtained by the Kriging surrogate model used in the prototype design process tested in this work. A flow analysis confirms the positive impact of the optimized casing groove design on the stage isentropic efficiency compared to the diffusion design and compared to the benchmark axisymmetric design. (C) 2018 The Authors. Published by Elsevier Ltd.
机译:基于计算机的优化技术的进步可用于提高能量转换过程的效率,例如通过减少火力发电厂涡轮机的空气动力损失。减少这种流动能量损失的一种可行方法是通过端壁轮廓加工。本文针对1.5级轴流式涡轮机的壳体几何形状实现了设计优化工作流程,以减少二次流。优化过程中使用了两种不同的参数化套管表面定义。第一种方法是使用新的表面定义进行新的非轴对称套管设计。第二种方法是已建立的扩散设计技术。这些设计在三维轴向涡轮RANS模型上进行了测试。演示了基于计算机的表面拓扑优化,可实现自动化的设计过程。这是使用自动化流程和优化工作台(APOW)软件实现的。克里金法用于加速优化过程。优化及其敏感性分析使人相信,通过在这项工作中测试的原型设计过程中使用的Kriging替代模型可以获得良好的预测能力。流量分析证实了与扩散设计和基准轴对称设计相比,优化的套管凹槽设计对阶段等熵效率的积极影响。 (C)2018作者。由Elsevier Ltd.发布

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